CN205714857U - A kind of antecurvature multiple wing type centrifugal blower fan - Google Patents

A kind of antecurvature multiple wing type centrifugal blower fan Download PDF

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CN205714857U
CN205714857U CN201620377353.8U CN201620377353U CN205714857U CN 205714857 U CN205714857 U CN 205714857U CN 201620377353 U CN201620377353 U CN 201620377353U CN 205714857 U CN205714857 U CN 205714857U
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impeller
volute
centrifugal fan
fan
diameter
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金守清
陈佑星
王倩
朱如洪
唐照付
张劲戈
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Yingfei Tongren Fan Co ltd
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Shanghai Nautilus General Equipment Manufacturing Co Ltd
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Abstract

本实用新型公开了一种前弯多翼式离心风机,包括蜗壳和叶轮;所述蜗壳包括蜗舌,及依次相切并光滑连接的第一弯曲表面、第二弯曲表面和第三弯曲表面;所述叶轮与所述蜗壳偏心设置用于使叶轮直径增大。本实用新型将叶轮相对蜗壳偏心安装增大了叶轮直径,明显提升风量风压等参数,降低了噪音,不会发生风机喘振,改善了风机性能;同时采用三段弧面构成蜗壳简化了蜗壳型线,节约空间体积,结构形式简单,无焊接工艺,加工成本低,使蜗壳制造更加方便。

The utility model discloses a forward-curved multi-blade centrifugal fan, which comprises a volute and an impeller; the volute comprises a volute, and sequentially tangent and smoothly connected first curved surface, second curved surface and third curved surface. Surface; the eccentric arrangement of the impeller and the volute is used to increase the diameter of the impeller. In the utility model, the eccentric installation of the impeller relative to the volute increases the diameter of the impeller, significantly improves parameters such as air volume and pressure, reduces noise, prevents fan surge, and improves the performance of the fan; The volute shape line is improved, the space volume is saved, the structure is simple, there is no welding process, the processing cost is low, and the volute manufacturing is more convenient.

Description

一种前弯多翼式离心风机A forward curved multi-blade centrifugal fan

技术领域technical field

本实用新型涉及空调通风领域,尤其涉及的是一种前弯多翼式离心风机,尤其适用于小型前弯多翼式双吸离心风机。The utility model relates to the field of air conditioning and ventilation, in particular to a forward-curved multi-blade centrifugal fan, which is especially suitable for a small forward-curved multi-blade double-suction centrifugal fan.

背景技术Background technique

多翼式离心通风机具有流量系数大、压力系数高、尺寸系数小以及噪音相对较低等优点,被广泛应用于空调行业中。前弯多翼式离心风机是离心式通风机的一种,属于叶片风机。这种风机叶轮的主要特点是采用轮径比大(0.8~0.95),相对宽度大(叶轮外径的0.4倍左右)的前弯叶片,而且叶片数量很多(32~64)。蜗壳进风口与叶轮为间隙式配合,轴向间隙值一般取叶轮外径的0.02~0.025倍。在多翼式离心风机中,通常采用内置电机,处于叶轮的中心区域,以节省空间。The multi-blade centrifugal fan has the advantages of large flow coefficient, high pressure coefficient, small size coefficient and relatively low noise, and is widely used in the air-conditioning industry. The forward curved multi-blade centrifugal fan is a kind of centrifugal fan and belongs to the blade fan. The main feature of this fan impeller is the use of forward curved blades with a large wheel diameter ratio (0.8~0.95), relatively large width (about 0.4 times the outer diameter of the impeller), and a large number of blades (32~64). The air inlet of the volute is fitted with the impeller in a gap type, and the axial gap value is generally 0.02~0.025 times the outer diameter of the impeller. In the multi-blade centrifugal fan, a built-in motor is usually used, which is located in the center area of the impeller to save space.

多翼式离心风机的这种特殊结构使得它的工作特点不同于其它形式的通风机。它的工作效率相对较低,在一定程度上限制了其使用范围。为提高多翼式离心风机的效率,将传统等厚度单圆弧直叶片改成翼型叶片、梯形叶片或扭曲叶片,但确定合理的优化方案却不容易实现,而且造成结构复杂、加工困难、成本过高,实用价值不大。The special structure of the multi-blade centrifugal fan makes its working characteristics different from other forms of fans. Its work efficiency is relatively low, which limits its scope of use to a certain extent. In order to improve the efficiency of the multi-blade centrifugal fan, the traditional equal-thickness single-arc straight blades are changed into airfoil blades, trapezoidal blades or twisted blades, but it is not easy to determine a reasonable optimization scheme, and it causes complex structures, difficult processing, The cost is too high and the practical value is not large.

空调用多翼式离心风机的蜗壳设计不能完全引用工业风机的设计方法和经验数据,叶轮与蜗壳几何中心重合未必是最佳安装位置,传统蜗壳型线也不一定是最合理的。然而,一些研究人员据此提出的蜗壳内壁型线二维设计理论、变螺旋角设计理论,又显得过于复杂,可操作性较差。The volute design of the multi-blade centrifugal fan for air conditioning cannot fully refer to the design methods and empirical data of industrial fans. The coincidence of the geometric center of the impeller and the volute may not be the best installation position, and the traditional volute profile may not be the most reasonable. However, the two-dimensional design theory of the inner wall of the volute and the variable helix angle design theory proposed by some researchers based on this are too complicated and poor in operability.

因此,现有技术还有待于改进和发展。Therefore, the prior art still needs to be improved and developed.

实用新型内容Utility model content

鉴于上述现有技术的不足,本实用新型的目的在于提供一种前弯多翼式离心风机,偏心设置叶轮和蜗壳,增大叶轮直径,采用三段弧面构成蜗壳简化了离心风机机构。In view of the above deficiencies in the prior art, the purpose of this utility model is to provide a forward curved multi-blade centrifugal fan, the impeller and volute are arranged eccentrically, the diameter of the impeller is increased, and the volute is formed by three sections of arc surface to simplify the mechanism of the centrifugal fan .

本实用新型的技术方案如下:The technical scheme of the utility model is as follows:

一种前弯多翼式离心风机,包括蜗壳和叶轮;A forward curved multi-blade centrifugal fan, including a volute and an impeller;

所述蜗壳包括蜗舌,及依次相切并光滑连接的第一弯曲表面、第二弯曲表面和第三弯曲表面;The volute includes a volute tongue, and a first curved surface, a second curved surface and a third curved surface which are sequentially tangent and smoothly connected;

所述叶轮与所述蜗壳偏心设置用于使叶轮直径D´增大。The eccentric arrangement of the impeller and the volute is used to increase the diameter D′ of the impeller.

进一步地,所述前弯多翼式离心风机中,所述叶轮与所述蜗壳同心设置的叶轮直径为D,偏心设置的叶轮直径D´=1.1D。Further, in the forward curved multi-blade centrifugal fan, the diameter of the impeller arranged concentrically with the volute is D, and the diameter of the impeller arranged eccentrically is D´=1.1D.

进一步地,所述前弯多翼式离心风机中,所述叶轮与所述蜗壳的偏心值L=(D´-D)/2。Further, in the forward curved multi-blade centrifugal fan, the eccentric value of the impeller and the volute is L=(D´-D)/2.

进一步地,所述前弯多翼式离心风机中,所述叶轮的轮径比为0.85,所述叶轮的相对宽度为0.75D。Further, in the forward curved multi-blade centrifugal fan, the wheel diameter ratio of the impeller is 0.85, and the relative width of the impeller is 0.75D.

进一步地,所述前弯多翼式离心风机中,所述叶轮的叶片数量为48。Further, in the forward curved multi-blade centrifugal fan, the number of blades of the impeller is 48.

本实用新型所提供的前弯多翼式离心风机,将叶轮相对蜗壳偏心安装增大了叶轮直径,离心风机功率随流量增大一直上升可过载,明显提升风量风压等参数,降低了噪音,不会发生风机喘振,改善了风机性能;同时采用三段弧面构成蜗壳简化了蜗壳型线,节约空间体积,结构形式简单,无焊接工艺,加工成本低,使蜗壳制造更加方便。The forward curved multi-blade centrifugal fan provided by the utility model installs the impeller eccentrically relative to the volute to increase the diameter of the impeller. The power of the centrifugal fan increases with the increase of the flow rate and can be overloaded. The parameters such as air volume and pressure are significantly improved, and the noise is reduced. , there will be no fan surge, and the performance of the fan is improved; at the same time, the three-section arc surface is used to form the volute to simplify the volute profile, save space and volume, the structure is simple, there is no welding process, and the processing cost is low, making the volute manufacturing more convenient. convenient.

附图说明Description of drawings

图1为传统无偏心的离心风机结构示意图。Figure 1 is a schematic structural diagram of a traditional non-eccentric centrifugal fan.

图2为传统四段圆弧的蜗壳结构示意图。Fig. 2 is a schematic diagram of a traditional four-segment arc volute structure.

图3为本实用新型的前弯多翼式离心风机的结构示意图。Fig. 3 is a structural schematic diagram of a forward-curved multi-blade centrifugal fan of the present invention.

图4为本实用新型的前弯多翼式离心风机中叶轮的结构示意图。Fig. 4 is a structural schematic diagram of the impeller in the forward curved multi-blade centrifugal fan of the present invention.

图5为本实用新型的前弯多翼式离心风机的风机流场分布效果图。Fig. 5 is an effect diagram of the fan flow field distribution of the forward curved multi-blade centrifugal fan of the present invention.

图6为本实用新型的前弯多翼式离心风机的实测性能曲线图。Fig. 6 is a measured performance curve of the forward-curved multi-blade centrifugal fan of the present invention.

具体实施方式detailed description

本实用新型提供一种前弯多翼式离心风机,为使本实用新型的目的、技术方案及效果更加清楚、明确,以下参照附图并举实例对本实用新型进一步详细说明。应当理解,此处所描述的具体实施例仅用以解释本实用新型,并不用于限定本实用新型。The utility model provides a forward-curved multi-blade centrifugal fan. In order to make the purpose, technical solution and effect of the utility model clearer and clearer, the utility model will be further described in detail below with reference to the accompanying drawings and examples. It should be understood that the specific embodiments described here are only used to explain the utility model, and are not intended to limit the utility model.

如图1所示,图1为传统无偏心的离心风机结构示意图,离心风机的蜗壳1的作用是将离开叶轮2的气体集中、导流,并将气体的部分动能扩压转变为静压。蜗壳1内壁型线如果设计不当,动能损失和噪音将增大,当离心风机偏离设计工况运行时尤其严重,叶轮2的直径为D。传统常规离心风机的叶轮2旋转中心与蜗壳1基方中心一致,即同心安装,其几何中心重合。传统常规离心风机的蜗壳1型线由四段圆弧近似而成,通常是等边基方或不等边基方。如图2所示,四段圆弧的半径分别为R1’、R2’、R3’和R4’。本实用新型设计思路基于保证风机性能不降低的前提下,优化风机结构,简化蜗壳1型线。即将蜗壳1内壁型线由传统的四段弧面缩减至三段相切弧面,蜗壳1尺寸相差不大,结构相对简易,且制造更加方便。As shown in Figure 1, Figure 1 is a schematic structural diagram of a traditional non-eccentric centrifugal fan. The function of the volute 1 of the centrifugal fan is to concentrate and guide the gas leaving the impeller 2, and to convert part of the kinetic energy of the gas into static pressure. . If the profile of the inner wall of the volute 1 is improperly designed, the kinetic energy loss and noise will increase, especially when the centrifugal fan deviates from the design working condition, and the diameter of the impeller 2 is D. The rotation center of the impeller 2 of the traditional conventional centrifugal fan is consistent with the base square center of the volute 1, that is, they are installed concentrically, and their geometric centers coincide. The type 1 line of the volute of a traditional conventional centrifugal fan is approximated by four arcs, usually an equilateral base square or a unequal base square. As shown in Figure 2, the radii of the four arcs are R1', R2', R3' and R4' respectively. The design concept of the utility model is based on the premise of ensuring that the performance of the fan is not reduced, optimizing the structure of the fan, and simplifying the volute 1-shaped line. That is to say, the profile of the inner wall of the volute 1 is reduced from the traditional four-section arc surface to three tangent arc surfaces, the size of the volute 1 is not much different, the structure is relatively simple, and the manufacture is more convenient.

请参阅图3,本实用新型提供的前弯多翼式离心风机,包括蜗壳1和叶轮2;与现有技术相比,叶轮2的直径增大为D’,本实用新型中所述的蜗壳1包括第一弯曲表面3(其半径为R1)、第二弯曲表面4(其半径为R2)和第三弯曲表面5(其半径为R3)和蜗舌,所述第一弯曲表面3、第二弯曲表面4和第三弯曲5的表面依次相切并光滑连接,采用三段弧面构成蜗壳1简化了蜗壳1型线,简化了传统四段圆弧近似成型的蜗壳1,使蜗壳1制造更加方便,零部件制造由模具成型,具有无焊接工艺,制造方便,加工成本低的优点。Please refer to Fig. 3, the forward curved multi-blade centrifugal fan provided by the utility model includes a volute 1 and an impeller 2; compared with the prior art, the diameter of the impeller 2 is increased to D', the utility model described The volute 1 comprises a first curved surface 3 (with a radius R1), a second curved surface 4 (with a radius R2) and a third curved surface 5 (with a radius R3) and a volute tongue, the first curved surface 3 , The surfaces of the second curved surface 4 and the third curved surface 5 are sequentially tangent and smoothly connected, and the three-section arc surface is used to form the volute 1, which simplifies the shape line of the volute 1, and simplifies the traditional four-section arc approximate molding volute 1 , so that the manufacture of the volute 1 is more convenient, and the parts are manufactured by moulding, which has the advantages of no welding process, convenient manufacture and low processing cost.

请参阅图2,图2为传统四段圆弧的蜗壳1结构示意图,传统常规离心风机的蜗壳1型线由四段圆弧近似而成,通常是等边基方或不等边基方。叶轮2是风机最终与气体介质接触并对其做功的部件,风机叶轮的主要结构参数包括叶轮外径、叶轮宽度、内外轮径比、叶片进出口安装角度、叶片数量等等,各个参数都会对风机性能产生影响。Please refer to Fig. 2, Fig. 2 is a schematic diagram of the structure of the volute 1 of the traditional four-segment arc. The volute 1 type line of the traditional conventional centrifugal fan is approximated by four arcs, which is usually an equilateral base square or a scalene base. square. The impeller 2 is the part of the fan that is finally in contact with the gas medium and does work on it. The main structural parameters of the fan impeller include the outer diameter of the impeller, the width of the impeller, the ratio of inner and outer wheel diameters, the installation angle of the blade inlet and outlet, the number of blades, etc. Fan performance is affected.

根据风机相似性定律,风量与叶轮直径成三次方关系,风压与叶轮直径成二次方关系,可见叶轮直径对风机性能的影响之大。但因一些实际需求,风机外形尺寸受限,不可增大。在风机性能不满足的情况下,若增大叶轮直径,蜗壳尺寸却不能同步放大,即选用同系列大机号风机不可取。如果直接放大叶轮直径,将导致蜗舌间隙过小,效率下降,噪音增大,因为蜗壳内部空间有限,上述方案亦不可实施。According to the law of fan similarity, the air volume has a cubic relationship with the diameter of the impeller, and the wind pressure has a quadratic relationship with the diameter of the impeller. It can be seen that the diameter of the impeller has a great influence on the performance of the fan. However, due to some actual needs, the size of the fan is limited and cannot be enlarged. If the performance of the fan is not satisfactory, if the diameter of the impeller is increased, the size of the volute cannot be enlarged simultaneously, that is, it is not advisable to use the same series of large-scale fans. If the diameter of the impeller is directly enlarged, the volute tongue clearance will be too small, the efficiency will decrease, and the noise will increase. Because the internal space of the volute is limited, the above scheme cannot be implemented.

如图3所示,本实用新型基于上述技术问题提出的增大叶轮直径的技术方案为:将离心风机中的所述叶轮2与所述蜗壳1偏心设置,以用于使叶轮2直径D´增大。本实用新型中叶轮2与蜗壳1的安装位置有一定偏心,保证了离心风机的外形尺寸和蜗舌间隙;即叶轮2向蜗壳1内侧偏移以增大叶轮2直径,叶轮2直径的增加可明显提升风量风压等性能参数,使风机效率得以提高,并降低了噪音水平,提高风机性能。As shown in Figure 3, the technical solution for increasing the diameter of the impeller proposed by the utility model based on the above-mentioned technical problems is: the impeller 2 and the volute 1 in the centrifugal fan are arranged eccentrically, so that the diameter of the impeller 2 is D ´ Increased. In the utility model, the installation position of the impeller 2 and the volute 1 has a certain eccentricity, which ensures the external dimensions and the volute tongue clearance of the centrifugal fan; that is, the impeller 2 is offset to the inner side of the volute 1 to increase the diameter of the impeller 2, and the diameter of the impeller 2 The increase can significantly improve performance parameters such as air volume and pressure, improve the efficiency of the fan, reduce the noise level, and improve the performance of the fan.

具体的,如图1和图3所示,传统离心风机的叶轮2与蜗壳1同心设置时的叶轮2直径为D,本实用新型的离心风机叶轮2与蜗壳1偏心设置后,偏心设置的叶轮2直径D´=1.1D;叶轮2与蜗壳1的偏心值L=(D´-D)/2。离心风机外形尺寸可以保持不变,叶片的形式也无需修改,即可改善离心风机的性能。Specifically, as shown in Figure 1 and Figure 3, when the impeller 2 of the traditional centrifugal fan is concentrically arranged with the volute 1, the diameter of the impeller 2 is D. The diameter of the impeller 2 D´=1.1D; the eccentric value of the impeller 2 and the volute 1 L=(D´-D)/2. The overall size of the centrifugal fan can be kept unchanged, and the form of the blade does not need to be modified, so the performance of the centrifugal fan can be improved.

进一步地,作为本实用新型的一个实施例,如图3和图4所示,本实用新型设置所述叶轮2的轮径比为0.85,设置所述叶轮2的相对宽度为0.75D,所述叶轮2的叶片数量为48。具有以上技术特征的离心风机,可明显提升风量风压等性能参数,使离心风机效率得以提高,并降低了离心风机的噪音水平。Further, as an embodiment of the present invention, as shown in Fig. 3 and Fig. 4, the present invention sets the wheel diameter ratio of the impeller 2 to 0.85, sets the relative width of the impeller 2 to 0.75D, and the The number of blades of the impeller 2 is 48. The centrifugal fan with the above technical features can significantly improve performance parameters such as air volume and pressure, improve the efficiency of the centrifugal fan, and reduce the noise level of the centrifugal fan.

将所述叶轮2的叶片设为等厚度单圆弧直叶片,使所述叶片呈刀刃状。The blades of the impeller 2 are set as single-arc straight blades of equal thickness, so that the blades are in the shape of blades.

请参阅图5和图6,图5为本实用新型的前弯多翼式离心风机的风机流场分布效果图。图中气流从离心风机两侧进风口进入到离心风机内部,经过叶轮2高速旋转,对其做功,再由出风口输送到指定工作区域,可直观认识到风机内部流体流动状况,流体密度大,且流动效率很高。图6为本实用新型的前弯多翼式离心风机的实测性能曲线图。图中四条曲线从上到下分别是:效率—流量曲线,功率—流量曲线,全压—流量曲线和静压—流量曲线。可看出,本实用新型的离心风机最高静压效率达到30%,在前弯多翼领域、电机内置情况下,相对良好;功率随流量增大一直上升,可过载;压力曲线较平缓,驼峰不明显,不会发生风机喘振;明显提升风量风压等性能参数的情况下降低了噪音水平,提高风机性能。Please refer to Fig. 5 and Fig. 6, Fig. 5 is an effect diagram of the fan flow field distribution of the forward curved multi-blade centrifugal fan of the present invention. In the figure, the air flow enters the centrifugal fan from the air inlets on both sides of the centrifugal fan, passes through the high-speed rotation of the impeller 2, does work on it, and is transported to the designated working area by the air outlet, so that the internal fluid flow of the fan can be intuitively recognized, and the fluid density is high. And the flow efficiency is very high. Fig. 6 is a measured performance curve of the forward-curved multi-blade centrifugal fan of the present invention. The four curves in the figure are from top to bottom: efficiency-flow curve, power-flow curve, total pressure-flow curve and static pressure-flow curve. It can be seen that the maximum static pressure efficiency of the centrifugal fan of the utility model reaches 30%, and it is relatively good in the field of forward-bending multi-wings and the built-in motor; the power increases with the increase of the flow rate, and it can be overloaded; It is not obvious, and there will be no fan surge; the noise level is reduced while the performance parameters such as air volume and pressure are significantly improved, and the performance of the fan is improved.

综上所述,本实用新型所提供的前弯多翼式离心风机,将叶轮相对蜗壳偏心安装增大了叶轮直径,离心风机功率随流量增大一直上升可过载,明显提升风量风压等参数,降低了噪音,不会发生风机喘振,改善了风机性能;同时采用三段弧面构成蜗壳简化了蜗壳型线,节约空间体积,结构形式简单,无焊接工艺,加工成本低,使蜗壳制造更加方便。To sum up, the forward curved multi-blade centrifugal fan provided by the utility model installs the impeller eccentrically relative to the volute to increase the diameter of the impeller, and the power of the centrifugal fan increases with the increase of the flow rate so that it can be overloaded, and the air volume and pressure can be significantly improved. parameters, reducing noise, no fan surge, and improved fan performance; at the same time, the three-section arc surface is used to form the volute to simplify the volute profile, save space and volume, simple structure, no welding process, low processing cost, Make the volute manufacturing more convenient.

应当理解的是,本实用新型的应用不限于上述的举例,对本领域普通技术人员来说,可以根据上述说明加以改进或变换,例如,所有这些改进和变换都应属于本实用新型所附权利要求的保护范围。It should be understood that the application of the present utility model is not limited to the above examples, and those of ordinary skill in the art can improve or change according to the above description, for example, all these improvements and changes should belong to the appended claims of the present utility model scope of protection.

Claims (5)

1.一种前弯多翼式离心风机,其特征在于,包括蜗壳和叶轮;1. A forward curved multi-blade centrifugal fan is characterized in that it comprises a volute and an impeller; 所述蜗壳包括蜗舌,及依次相切并光滑连接的第一弯曲表面、第二弯曲表面和第三弯曲表面;The volute includes a volute tongue, and a first curved surface, a second curved surface and a third curved surface which are sequentially tangent and smoothly connected; 所述叶轮与所述蜗壳偏心设置,偏心设置后的叶轮直径大于同心设置的叶轮直径。The impeller is arranged eccentrically with the volute, and the diameter of the impeller after the eccentric arrangement is larger than that of the impeller arranged concentrically. 2.根据权利要求1所述的前弯多翼式离心风机,其特征在于,所述叶轮与所述蜗壳同心设置的叶轮直径为D,偏心设置的叶轮直径D´=1.1D。2. The forward-curved multi-blade centrifugal fan according to claim 1, wherein the diameter of the impeller arranged concentrically with the volute is D, and the diameter of the impeller arranged eccentrically is D´=1.1D. 3.根据权利要求2所述的前弯多翼式离心风机,其特征在于,所述叶轮与所述蜗壳的偏心值L=(D´-D)/2。3. The forward-curved multi-blade centrifugal fan according to claim 2, wherein the eccentric value of the impeller and the volute is L=(D´-D)/2. 4.根据权利要求3所述的前弯多翼式离心风机,其特征在于,所述叶轮的轮径比为0.85,所述叶轮的相对宽度为0.75D。4 . The forward curved multi-blade centrifugal fan according to claim 3 , wherein the wheel diameter ratio of the impeller is 0.85, and the relative width of the impeller is 0.75D. 5.根据权利要求4所述的前弯多翼式离心风机,其特征在于,所述叶轮的叶片数量为48。5 . The forward-curved multi-blade centrifugal fan according to claim 4 , wherein the number of blades of the impeller is 48. 6 .
CN201620377353.8U 2016-04-29 2016-04-29 A kind of antecurvature multiple wing type centrifugal blower fan Expired - Lifetime CN205714857U (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105715570A (en) * 2016-04-29 2016-06-29 上海诺地乐通用设备制造有限公司 Forward-curved multi-wing type centrifugal fan
CN113221484A (en) * 2021-06-02 2021-08-06 上海宝钢节能环保技术有限公司 Rapid selection method, device and equipment for in-service remanufacturing design scheme of fan

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105715570A (en) * 2016-04-29 2016-06-29 上海诺地乐通用设备制造有限公司 Forward-curved multi-wing type centrifugal fan
CN113221484A (en) * 2021-06-02 2021-08-06 上海宝钢节能环保技术有限公司 Rapid selection method, device and equipment for in-service remanufacturing design scheme of fan
CN113221484B (en) * 2021-06-02 2022-11-11 上海宝钢节能环保技术有限公司 Rapid selection method, device and equipment for in-service remanufacturing design scheme of fan

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